# NTSB FTW03LA026: Cessna 177RG, N35866, Marshall, AR, October 31, 2002

- Type: NTSB accident investigation
- Classification: Accident · Minor injuries · Limited investigation · Final report
- Date: October 31, 2002, 11:10 local (17:10 UTC)
- Place: Marshall, AR
- Coordinates: 35.898612, -92.659721
- Nearby events: https://openairdocs.org/map.md?lat=35.8986&lon=-92.6597&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: Minor injuries
- Injuries: 1 minor
- Status: Completed, report July 23, 2003
- Report: Approved by Office Director
- Parties: Federal Aviation Administration
- NTSB case key (mKey): 55982
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=FTW03LA026
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/55982/pdf
- Page: https://openairdocs.org/ntsb/FTW03LA026

## Probable cause

The loss of engine power for undetermined reasons.  A contributing factor was the lack of suitable terrain for the forced landing.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Loss of engine power, cruise
  - reason for occurrence undetermined (cause)
- Forced landing, descent - emergency
- On ground/water encounter with terrain/water, emergency landing
  - terrain condition - ditch
  - terrain condition - none suitable (contributing factor)
- Nose over, emergency landing

## Analysis

Approximately 5 miles from the departure airport, the engine started to lose power.  The pilot turned the airplane back toward the airport; however, the engine regained power, and the pilot elected to continue the flight.  Approximately 25 minutes later, the engine gradually lost power, then after 2 minutes, the engine lost total power.  In an attempt to regain engine power, the pilot checked the magnetos, fuel boost pump, and adjusted the throttle, mixture, and propeller settings.  Unable to restart the engine, the pilot initiated a forced landing to a field.  During the forced landing, the airplane struck a ditch, flipped over, and came to rest inverted.  No anomalies were noted during an examination of the engine and airframe.  The engine was test run at various low power settings with no anomalies noted.  The reason for the total loss of engine power was not determined.

## Factual narrative

On October 31, 2002, at 1110 central standard time, a Cessna 177RG single-engine airplane, N35866, sustained substantial damage during a forced landing following a loss of engine power during cruise flight near Marshall, Arkansas.  The commercial pilot, sole occupant of the airplane, sustained minor injuries.  The airplane was registered to and operated by RAS Inc., of Deland, Florida.  Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 positioning flight.  The flight departed the Carroll County Airport, Berryville, Arkansas, approximately 1040, with an intended destination of Clinton, Arkansas.

In a telephone interview conducted by the NTSB investigator-in-charge (IIC), the pilot reported that approximately 5 miles from the Carroll County Airport, the engine started to lose power.  The pilot turned the airplane back toward the airport; however, the engine regained power, and the pilot elected to continue the flight.  Approximately 25 minutes later, while in cruise flight at 3,000 feet mean sea level (msl), the engine gradually lost power, then after 2 minutes, the engine lost total power.  In an attempt to regain engine power, the pilot checked the magnetos, fuel boost pump, and adjusted the throttle, mixture, and propeller settings.  Unable to restart the engine, the pilot initiated a forced landing to a field.  During the forced landing, the airplane struck a ditch, nosed over, and came to rest inverted.  The pilot added that the airplane's fuel tanks contained approximately 2.5 hours of fuel at the time of departure.

According to an FAA inspector, the left and right wing spars and rudder sustained structural damage.

On November 2, 2002, an FAA inspector examined the airframe and engine at a facility in Berryville.  The inspector reported that he rotated the propeller through several times, and the rotation was "smooth and normal."  The inspector checked the fuel for contamination, and no anomalies were noted with fuel sample.

On November 6, 2002, at the facility in Berryville, under the supervision of an FAA inspector, the airframe and engine were visually examined and an engine test-run was conducted.  No anomalies were noted with the engine.  The engine started on the first attempt and was operated for approximately three minutes.  During the engine test run, the throttle was advanced to approximately 1,000-1,100 revolutions per minute (rpm), and then decreased to 900 rpms, no hesitation or lag was noted.  The mixture control was then moved to almost full aft (lean) and the power reduced with no hesitation or lag.  The mixture control was then moved to full forward (rich), and the power increased back to 900 rpms with no hesitation or lag noted.  No anomalies were noted during the engine test run.

The engine logbooks revealed that the Lycoming IO-360-A1B6D engine, serial number, L-16456-51A, most recent annual inspection was completed on October 30, 2002, at a tachometer time of 2,014.2 hours.  In addition, a major overhaul to the engine was completed on October 29, 2002, at a tachometer time of 2,041.2 hours.  The recorded tachometer time at the accident site was 2,042.2 hours.

The reason for the total loss of engine power was not determined.

## Aircraft

- Registration: [N35866](https://openairdocs.org/aircraft/N35866), registered now, S/N 177RG1065, built 1976 (OpenAirDocs)
- Reported make and model: Cessna 177RG
- Registry model: [Cessna 177RG](https://openairdocs.org/model/cessna-177rg) (registry code 2073709) (OpenAirDocs)
- Registry engine: [Lycoming IO-360-A1B6D](https://openairdocs.org/engine/lycoming-io-360-a1b6d) (registry code 41593, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 177RG1065
- Airframe hours: 2042
- Engines: Lycoming IO-360-A1B6D 210 horsepower reciprocating
- Damage: Substantial damage
- Flight: Positioning, Part 91
- Registered owner: RAS Inc.
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, October 30, 2002, 3 hours before
- Departed: 4M1, Berryville, AR
- Destination: 4M4, Clinton, AR

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 49; injuries: minor; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; last flight review February 3, 2001; seat: left; flight hours: 1,405 total, 48 in this make and model, 1,260 as pilot in command, 170 in the last 90 days, 81 in the last 30 days, 2 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 300° at 15 knots
- Visibility: 10 statute miles
- Lowest ceiling: 1,500 ft broken
- Temperature: 39 °F

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20021031031349A](https://openairdocs.org/incident/20021031031349A), Oct 31, 2002: Cessna 177RG, Marshall, AR, Substantial damage. (-23) On October 31, 2002, at 1110 central standard time, a Cessna 177RG, registration number N35866, serial number 177RG1065 while being operated by…

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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